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High Temperature Material Processes: An International Quarterly of High-Technology Plasma Processes
SJR: 0.137 SNIP: 0.341 CiteScore™: 0.43

ISSN Печать: 1093-3611
ISSN Онлайн: 1940-4360

Выпуски:
Том 23, 2019 Том 22, 2018 Том 21, 2017 Том 20, 2016 Том 19, 2015 Том 18, 2014 Том 17, 2013 Том 16, 2012 Том 15, 2011 Том 14, 2010 Том 13, 2009 Том 12, 2008 Том 11, 2007 Том 10, 2006 Том 9, 2005 Том 8, 2004 Том 7, 2003 Том 6, 2002 Том 5, 2001 Том 4, 2000 Том 3, 1999 Том 2, 1998 Том 1, 1997

High Temperature Material Processes: An International Quarterly of High-Technology Plasma Processes

DOI: 10.1615/HighTempMatProc.v1.i4.100
pages 525-533

MODELLING OF THE HEAT TRANSFER DURING OXYGEN ATOMS RECOMBINATION ON METALLIC SURFACES IN A PLASMA REACTOR

S. Cavadias
Laboratoire Genie Precedes Plasmas - ENSCP 11, rue Pierre et Marie Curie - 75005 Paris- France
M. Van Der Zwan
Dept of Chemical Engineering - University of Rijks - Groninghen Nijenborg 4 - 9747 AG Groninghen - The Nederlands
P. Cauquot
Laboratoire de Genie des Procedes Plasmas et Traitement de Surface - ENSCP -11, rue Pierre et Marie Curie - 75231 Paris Cedex 05
Jacques Amouroux
Laboratoire de Genie des Precedes Plasmas Universite P. et M. Curie, ENSCP 11 rue P. et M. Curie 75005 Paris France

Краткое описание

Space shuttle overheating during the re-entry phase, due to catalytic oxygen recombination on the thermal protection system, is a problem of practical and theoretical interest. The energy transfer is characterised by the product of the accommodation and the recombination coefficients. Previous measurements of recombination coefficient "gamma" on the metallic samples allowed the establishment of a catalycity scale. The purpose of this work is the modelling of the recombination of oxygen atoms and transfer of the energy to a metallic surface at stagnation point configuration by using a fluid dynamics code. The flow is described by a system of conservation (momentum, species and energy) equations. The necessary boundary conditions were provided by a model for a reactive flow-surface interaction. Under conditions similar to the experiment the field velocity, temperature and the fluxes of atomic and molecular oxygen in the reactor have been obtained. Assuming surface recombination of oxygen atoms only, the "gamma" coefficient was deduced from the ratios of atomic and molecular fluxes to the surface. The comparison of calculated values of "gamma" with the experimental ones leads to the determination of the surface recombination rate constant.


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